2012
DOI: 10.1016/j.corsci.2011.09.025
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Effect of prior corrosion state on the fatigue small cracking behaviour of 6151-T6 aluminum alloy

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Cited by 66 publications
(44 citation statements)
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“…The environmental effect on the fatigue fracture of 25CrMo axle steel not only depends on the formation of corrosive pits and solution exposure time but also depends on the local deformation of the metal (stress level). The former involves the transformation of corrosion pits to stress corrosion cracks and the latter involves a electrochemical process (anodic dissolution) and hydrogen embrittlement due to the cyclic deformation on the surface [26,[31][32][33]. In addition, there is some scatter in the corrosive fatigue data, including the fatigue data for the samples tested in air, as shown in Figure 3.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…The environmental effect on the fatigue fracture of 25CrMo axle steel not only depends on the formation of corrosive pits and solution exposure time but also depends on the local deformation of the metal (stress level). The former involves the transformation of corrosion pits to stress corrosion cracks and the latter involves a electrochemical process (anodic dissolution) and hydrogen embrittlement due to the cyclic deformation on the surface [26,[31][32][33]. In addition, there is some scatter in the corrosive fatigue data, including the fatigue data for the samples tested in air, as shown in Figure 3.…”
Section: Resultsmentioning
confidence: 99%
“…This is because the fatigue fracture life depends primarily on the inside crack propagation length (a) in the environmental fatigue condition. A greater inside crack propagation length indicates a stronger stress-corrosion coupling effect [26,[31][32][33]35]. Therefore, the probability of the corrosion solution acting on the surface crack at the multi-crack initiation sites is lower than it acting on the single crack initiation sites.…”
Section: Fractography Analysismentioning
confidence: 99%
“…However, it is widely accepted that corrosion fatigue crack initiation points are due to surface defects (such as corrosion pits and voids) of aluminium alloys caused by NaCl aqueous solutions by previous literature. 10,[13][14][15]27,28 In addition, effects of second cracks of high-strength aluminium alloy, 7475-T7351 and 7075-T651, as shown in Fig. 2a and b, and voids of high-ductility aluminium alloys, LY12-CZ and 2024-T4, as shown in Fig.…”
Section: R E S U L T S a N D Discussion Smentioning
confidence: 99%
“…All fatigue data for the different environmental media are plotted in Figure 3 involves the transformation of corrosion pits to stress corrosion cracks and the latter involves a electrochemical process (anodic dissolution) and hydrogen embrittlement due to the cyclic deformation on the surface [23,[27][28][29]. In addition, there is some scatter in the corrosive fatigue data, including the fatigue data for the samples tested in air, as shown in Figure 3.…”
Section: Resultsmentioning
confidence: 99%
“…This is because the fatigue fracture life depends primarily on the inside crack propagation length (a) in the environmental fatigue condition. A greater inside crack propagation length indicates a stronger stress-corrosion coupling effect [23,[27][28][29]31].…”
Section: Fractography Analysismentioning
confidence: 99%